Private Pilot Course - Ground Portion - Oral Exam
- Knowledge Exam - Computerized Exam
- Oral Exam - With Examination
- Practical Exam - Fly the Flight Plan, Diversion, Maneuvers, Under hood
Required Documents
- Student Pilot Certificate
- Medical Certificate
- Government Issued Photo ID
- Log Book
- Knowledge Test Results
- Hours
- Takeoffs
- Landings
- Flight Distances Required
Instructor Endorsements in Logbook Verify Sec 61.107 and Verify Sec 61.105
ICARA Integrated Airman Certification and Rating Application (On Line)
Pilot's Bill of Rights, Electronic Sign . Validate ID.
1. Plan A VFR Flight, Fuel, Weight and Balance
2. Airplane
ARROW (Airworthiness, Registration, Radio, Operating Limits, Weight and Balance)
Engine / Airplane Logs
Inspection -
Last 100 hours inspection
Transponder Test
ELT Battery
ELT 12 months inspection
Registration
Mark with TABS -
AD Note - FAA Airworthiness Directive Recurring done in log in log book
Annual Inspection - Airplane logbook / Airframe Log book
To take passenger 3 take off and landing within 90 days
1 every 24 calendar month
Night - 3 take off and landing with 90 days to a full stop
sunset and sun
3. Weather for the Flight -
Forecast of destination airport - Terminal Area Forecast
Winds Alof on Flight path 3,000' 6,000 Temperature /Winds
Nodams - Notice to Airman things out broken, closed
Weather Charts - Weather depiction - Ares of IFR marginal VFR,
Radar Summary - Precipitation
Weather Prog Chart - 4 panel forecast surface weather, weather to 24,000'
Sigmet - Signaficant - sever s
Airmet - lighter turbulence / freezing lev
Convective Signemt -
Windshare airport - Use Higher indicator airspeed
4. POH -
Use of Charts - Take off distance problem (performance Section)
Gross weight - Lift off speed / higher pressure altitude (altitude at standard 29.92) elevation and temperature (use warmer temperature) Ground roll 50' Obstacle
Cruse Performance - 70% Power True Airspeed / fuel consumption GPH
Temperature At 8,000' True Airspeed 140 Knots True .. Calibrated Airspeed
Head Wind/Tail Wind component
Landing Distance Problem -
23:00mins
Higher Distance Altitude - Use of Flaps
Density altitude is pressure altitude corrected by non standard temperature -
The higher the density altitude the worst the aircraft will perform
Temperature 90 deg outside 6,100' 29.93 - densitity altitude 10,000' - aircraft will perform at 10,000 feet ... poor performance
5. Weight and Balance
Moments arm CG envelope
https://www.youtube.com/watch?v=kr483zBbQKw
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